View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00082U 26152.17269914 +.00000000 +00000-0 +19196-3 0 00007
2 00082 38.8563 59.2671 1166148 148.5729 219.0284 12.27909589 06
| Epoch (UTC): | 01 June 2026 04:08:41 |
| Eccentricity: | 0.1166148 |
| inclination: | 38.8563° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 59.2671° |
| argument of perigee: | 148.5729° |
| revolutions per day: | 12.27909589 |
| mean anomaly at epoch: | 219.0284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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